The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 29, 2009

Filed:

Jun. 06, 2005
Applicants:

David Glenn Cherry, Loveland, OH (US);

Robert John Beacock, Cincinnati, OH (US);

William Larson Clifford, Cincinnati, OH (US);

Robert Joseph Orlando, West Chester, OH (US);

Thomas Ory Moniz, Loveland, OH (US);

Ching-pang Lee, Cincinnati, OH (US);

Inventors:

David Glenn Cherry, Loveland, OH (US);

Robert John Beacock, Cincinnati, OH (US);

William Larson Clifford, Cincinnati, OH (US);

Robert Joseph Orlando, West Chester, OH (US);

Thomas Ory Moniz, Loveland, OH (US);

Ching-Pang Lee, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/067 (2006.01); F02K 3/072 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turbofan engine includes a fan, compressor, combustor, high pressure turbine, and low pressure turbine joined in serial flow communication. The high pressure turbine includes two stages of rotor blades to effect corresponding exit swirl in the combustion gases discharged therefrom. A transition duct includes fairings extending between platforms for channeling the combustion gases to the low pressure turbine with corresponding swirl. First stage rotor blades in the low pressure turbine are oriented oppositely to the rotor blades in the high pressure turbine for counterrotation.


Find Patent Forward Citations

Loading…